The Generation of Inter-Element-Compatible Stiffness and Mass Matrices by the Use of Interpolation Formulas

Item

Title
The Generation of Inter-Element-Compatible Stiffness and Mass Matrices by the Use of Interpolation Formulas
Description
This paper presents a general method of subelement displacement states which makes it a relatively simple task to insure completely compatible displacement states. The method involves the use of Hermite interpolation formulas of various order. The total potential energy principle is used to generate stiffness matrices based on these displacement states. The approach is presented in general orthogonal curvilinear coordinates for shell type structures. Inter-element-compatible stiffness matrices are presented for a rectangular membrane, a rectangular plate with twelve degrees of freedom, and a rectangular plate with twenty four degrees of freedom. The corresponding consistent mass matrices are presented for both plate elements. Numerical examples of static deflection analysis are presented based on both of the plate subelements and the monotonic convergence of the discretization error is confirmed. Application of the simpler plate subelement to the determination of natural modes and frequencies is also illustrated with a numerical example. All of the examples are selected so that comparison with classical results can be made.
Date
1966
Index Abstract
Not Available
Photo Quality
Not Needed
Report Number
AFFDL-TR-66-80 p. 395-443
Creator
Bogner, F. K
Fox, R. L.
Schmit, L. A., Jr.
Corporate Author
Case Institute of Technology
Laboratory
Air Force Flight Dynamics Laboratory
Extent
49
Access Rights
Distribution of this document is unlimited.
Distribution Classification
1
Contract
Laboratory Research - No Contract
DTIC Record Exists
No
Distribution Change Authority Correspondence
None
Distribution Conflict
No
Report Availability
Full text available
Date Issued
1966-11
Abstract
This paper presents a general method of subelement displacement states which makes it a relatively simple task to insure completely compatible displacement states. The method involves the use of Hermite interpolation formulas of various order. The total potential energy principle is used to generate stiffness matrices based on these displacement states. The approach is presented in general orthogonal curvilinear coordinates for shell type structures. Inter-element-compatible stiffness matrices are presented for a rectangular membrane, a rectangular plate with twelve degrees of freedom, and a rectangular plate with twenty four degrees of freedom. The corresponding consistent mass matrices are presented for both plate elements. Numerical examples of static deflection analysis are presented based on both of the plate subelements and the monotonic convergence of the discretization error is confirmed. Application of the simpler plate subelement to the determination of natural modes and frequencies is also illustrated with a numerical example. All of the examples are selected so that comparison with classical results can be made.
Identifier
AD0646300
Provenance
Bombardier/Aero
Type
article
Format
1 online resource
Is Referenced By
Ummels, Raphael, & Castro, Saullo G. P. "Overlap-Stiffened Panels for Optimized Buckling Performance Under Minimum Steering Radius Constraints", Preprint DOI
10.31224/osf.io/xpvn4
Mauricio F. Caliri, Jr., Antonio J.M. Ferreira, and Volnei Titac
A new C1 4-node flat laminated shell element based on a generalized plate formulation
v163 (2021): 107648
[Oxford] : Elsevier Applied Science
Wang, Zhihua, José Humberto S. Almeida Jr., Aravind Ashok, Zhonglai Wang and Saullo G. P. Castro, "Lightweight design of variable-angle filament-wound cylinders combining Kriging-based metamodels with particle swarm optimization", May 12, 2021
https://engrxiv.org/3ym95/
Ummels, R., & Castro, S. G. P. (2021). Overlap-stiffened panels for optimized buckling performance under
minimum steering radius constraints. Composites Part C: Open Access, 6, [100174].
https://doi.org/10.1016/j.jcomc.2021.100174
Castro, S. G. P. & Jansen, E. L. (2022) Displacement-based multi-modal formulation of Koiter’s method applied to cylindrical shells. Preprint files.osf.io
Castro, S. G. P. & Jansen, E. L. (2022) Displacement-based multi-modal formulation of Koiter’s method applied to cylindrical shells AIAA SCITECH 2022 Forum https://arc.aiaa.org/doi/10.2514/6.2022-0256
Wang, Zhihua, José Humberto S. Almeida Jr., Aravind Ashok, Zhonglai Wang and Saullo G. P. Castro, "Lightweight design of variable-angle filament-wound cylinders combining Kriging-based metamodels with particle swarm optimization", Structural and Multidisciplinary Optimizaion, 65:140 (2022)

Linked resources


Warning: Undefined array key "id_concat" in /var/www/html/omeka-s/themes/foundation/view/common/linked-resources.phtml on line 40

Warning: Undefined array key "property_alternate_label" in /var/www/html/omeka-s/themes/foundation/view/common/linked-resources.phtml on line 41

Warning: Undefined array key "property_label" in /var/www/html/omeka-s/themes/foundation/view/common/linked-resources.phtml on line 43
Items with "Has Part: The Generation of Inter-Element-Compatible Stiffness and Mass Matrices by the Use of Interpolation Formulas"
Title Class
Matrix Methods in Structural Mechanics